CN101903238B - 包括加劲件边缘接合部的飞行器结构 - Google Patents

包括加劲件边缘接合部的飞行器结构 Download PDF

Info

Publication number
CN101903238B
CN101903238B CN200880121489.0A CN200880121489A CN101903238B CN 101903238 B CN101903238 B CN 101903238B CN 200880121489 A CN200880121489 A CN 200880121489A CN 101903238 B CN101903238 B CN 101903238B
Authority
CN
China
Prior art keywords
panel
stiffener
covering
multiplication part
shield
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN200880121489.0A
Other languages
English (en)
Chinese (zh)
Other versions
CN101903238A (zh
Inventor
海伦妮·卡泽纳夫
让·克劳德·拉孔布
布鲁诺·卡恰圭拉
大卫·安迪萨克
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Airbus Operations SAS
Original Assignee
Airbus Operations GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of CN101903238A publication Critical patent/CN101903238A/zh
Application granted granted Critical
Publication of CN101903238B publication Critical patent/CN101903238B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Braking Arrangements (AREA)
  • Connection Of Plates (AREA)
  • Gasket Seals (AREA)
CN200880121489.0A 2007-10-18 2008-09-12 包括加劲件边缘接合部的飞行器结构 Expired - Fee Related CN101903238B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0758423A FR2922518B1 (fr) 2007-10-18 2007-10-18 Structure d'avion comportant des jonctions d'arrets de raidisseurs
FR0758423 2007-10-18
PCT/FR2008/051631 WO2009050358A2 (fr) 2007-10-18 2008-09-12 Structure d'avion comportant des jonctions d'arrêts de raidisseur

Publications (2)

Publication Number Publication Date
CN101903238A CN101903238A (zh) 2010-12-01
CN101903238B true CN101903238B (zh) 2014-02-19

Family

ID=39473882

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200880121489.0A Expired - Fee Related CN101903238B (zh) 2007-10-18 2008-09-12 包括加劲件边缘接合部的飞行器结构

Country Status (10)

Country Link
US (1) US8215584B2 (fr)
EP (1) EP2209711B1 (fr)
JP (1) JP5250039B2 (fr)
CN (1) CN101903238B (fr)
AT (1) ATE555009T1 (fr)
BR (1) BRPI0817838A2 (fr)
CA (1) CA2702908C (fr)
FR (1) FR2922518B1 (fr)
RU (1) RU2433064C1 (fr)
WO (1) WO2009050358A2 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2922518B1 (fr) * 2007-10-18 2010-04-23 Airbus France Structure d'avion comportant des jonctions d'arrets de raidisseurs
FR2947522B1 (fr) 2009-07-03 2011-07-01 Airbus Operations Sas Element de fuselage comportant un troncon de fuselage et des moyens de jonction, portion de fuselage, fuselage et aeronef
ES2392236B1 (es) * 2010-01-15 2013-10-09 Airbus Operations, S.L. Componente de aeronave con paneles rigidizados con larguerillos.
DE102010013370B8 (de) 2010-03-30 2013-12-12 Eads Deutschland Gmbh Wandbauteil für ein Luftfahrzeug
EP2404824B1 (fr) * 2010-07-08 2015-09-09 Airbus Opérations SAS Structure d'aeronef et Procédé de réalisation d'une telle structure
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
FR2984845B1 (fr) * 2011-12-21 2014-07-11 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
US8960606B2 (en) * 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
ES2819076T3 (es) * 2013-04-30 2021-04-14 Airbus Operations Sl Estructura compuesta para una aeronave y procedimiento de fabricación de la misma
US10421528B2 (en) 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
US10207789B2 (en) * 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US20200122816A1 (en) * 2018-10-22 2020-04-23 The Boeing Company Bulkhead joint assembly
FR3114574A1 (fr) * 2020-09-30 2022-04-01 Airbus Operations Élément d’interface pour connecter deux tronçons de fuselage d’aéronef avec un nombre réduit de pièces.

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
WO2006001859A1 (fr) * 2004-04-06 2006-01-05 The Boeing Company Panneaux structurels destines a etre utilise dans des fuselages d'aeronefs
EP1719698A1 (fr) * 2005-05-05 2006-11-08 Northrop Grumman Corporation Isolation thermique d'un joint d'une structure effilée

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR2922518B1 (fr) * 2007-10-18 2010-04-23 Airbus France Structure d'avion comportant des jonctions d'arrets de raidisseurs
FR2922517B1 (fr) * 2007-10-18 2010-04-23 Airbus France Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
WO2006001859A1 (fr) * 2004-04-06 2006-01-05 The Boeing Company Panneaux structurels destines a etre utilise dans des fuselages d'aeronefs
EP1719698A1 (fr) * 2005-05-05 2006-11-08 Northrop Grumman Corporation Isolation thermique d'un joint d'une structure effilée

Also Published As

Publication number Publication date
CN101903238A (zh) 2010-12-01
ATE555009T1 (de) 2012-05-15
US8215584B2 (en) 2012-07-10
CA2702908A1 (fr) 2009-04-23
FR2922518A1 (fr) 2009-04-24
EP2209711B1 (fr) 2012-04-25
WO2009050358A3 (fr) 2009-06-11
FR2922518B1 (fr) 2010-04-23
JP2011500416A (ja) 2011-01-06
CA2702908C (fr) 2013-01-08
WO2009050358A2 (fr) 2009-04-23
BRPI0817838A2 (pt) 2015-03-31
US20100264272A1 (en) 2010-10-21
EP2209711A2 (fr) 2010-07-28
RU2433064C1 (ru) 2011-11-10
JP5250039B2 (ja) 2013-07-31

Similar Documents

Publication Publication Date Title
CN101903238B (zh) 包括加劲件边缘接合部的飞行器结构
CN101896399B (zh) 包括加劲件边缘接合部的飞行器及制造这种飞行器的方法
US8302909B2 (en) Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage
US8960606B2 (en) Circumference splice for joining shell structures
US7837148B2 (en) Composite wing-body joint
US20180237150A1 (en) Quick installation fuel dam
WO2020107532A1 (fr) Structure de liaison pour relier un longeron d'aile d'aéronef en matériau composite à une région d'emplanture
US10308345B2 (en) Structure
US9216811B2 (en) Aircraft comprising an improved connection zone between a front beam and a front lower fuselage section
US9862477B2 (en) Aircraft structure
RU2421375C2 (ru) Крыло самолета, панель крыла самолета и самолет
US20100127127A1 (en) Assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft
US7810758B2 (en) Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft
CN102616366A (zh) 用于加强位于飞行器机身与翼盒之间的框架的连接器
JP2016128314A (ja) 構造部品を接合するためのスプライスアセンブリ
US8679616B2 (en) Skew-angle radius filler
US10035586B2 (en) Aircraft wing with wing tip device
CN104724279A (zh) 用于飞行器升力面的前缘
US9868508B2 (en) Rib foot for aircraft wing
EP2626291B1 (fr) Joint structurel comprenant une peau en continu avec des lisees d'attache montées aux surfaces intérieure et extérieure
US20120025023A1 (en) Longitudinal junction for aircraft fuselage panels in composite materials
US10364017B2 (en) Structural component
US20150183508A1 (en) Horizontal tail plane of an aircraft

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140219

Termination date: 20200912

CF01 Termination of patent right due to non-payment of annual fee